View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10664U 26106.22797669 +.00000000 +00000-0 +84415-4 0 00009
2 10664 65.3760 21.1819 1899364 29.3604 340.1693 10.75899356 01
| Epoch (UTC): | 16 April 2026 05:28:17 |
| Eccentricity: | 0.1899364 |
| inclination: | 65.3760° |
| perigee height: | 643 km |
| apogee height: | 3935 km |
| right ascension of ascending node: | 21.1819° |
| argument of perigee: | 29.3604° |
| revolutions per day: | 10.75899356 |
| mean anomaly at epoch: | 340.1693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|